N3682L

Substantial
None

CESSNA 172GS/N: 17253851

Accident Details

Date
Saturday, April 20, 2013
NTSB Number
CEN13LA232
Location
Reading, MI
Event ID
20130422X94100
Coordinates
41.840000, -84.704170
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The partial loss of engine power due to the improper securing of the throttle linkage by maintenance personnel.

Aircraft Information

Registration
Make
CESSNA
Serial Number
17253851
Engine Type
Reciprocating
Year Built
1965
Model / ICAO
172GC172
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
4
FAA Model
172G

Registered Owner (Current)

Name
RISEAERO LLC
Address
PO BOX 13496
City
FLORENCE
State / Zip Code
SC 29504-3496
Country
United States

Analysis

On April 20, 2013, at 1130 eastern daylight time, a Cessna model 172G airplane, N3682L, was substantially damaged during a forced landing following a partial loss of engine power during cruise flight near Reading, Michigan. The airline transport pilot was not injured. The airplane was registered to and operated by a private individual, under the provisions of 14 Code of Federal Regulations Part 91, without a flight plan. Day visual meteorological conditions prevailed for the personal flight that departed Lenawee County Airport (KADG), Adrian, Michigan, at 1100, and was destined for Joliet Regional Airport (KJOT), Joliet, Illinois.The pilot reported that about 30 minutes into the cross-country flight, at 2,500 feet mean sea level, the engine speed inexplicably decreased from the selected cruise power setting to 1,900 rpm over a few seconds. The pilot was unable to restore full engine power and performed an off-airport landing in a nearby agricultural field. The airplane came to an abrupt stop when it encountered an area of deep mud during the landing. The main wing spar was substantially damaged when the right wingtip impacted terrain during the abrupt stop.

Maintenance inspectors with the Federal Aviation Administration examined the airplane before it was recovered from the accident site. Visual inspection of the engine compartment revealed that the throttle control had separated from the carburetor's throttle arm. The corresponding retention hardware was not recovered during the investigation. The engine recording tachometer indicated 3,078.96 hours at the accident site.

According to maintenance logbook information, the airplane had undergone an annual/100-hour inspection two days before the accident flight at 3,078.40 hours tachometer time. The aviation mechanic that performed the inspection, who also held an inspection authorization certificate, reported that after completing a field overhaul of the engine he could not locate the cotter-pin used to safety the airframe throttle control to the carburetor throttle arm. The mechanic elected to use safety wire to secure the throttle control assembly instead of the specified cotter-pin.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA232